Barrier layer measures to effect a barrier layer in a flow-past area of an aircraft's fuselage, support wing and tail plane has multiple laser beams to intersperse a flow boundary layer without gaps

摘要

First laser sources (7a) intersperse a flow-past area (5a) on an aircraft's fuselage nose (5). Second laser sources (7b) intersperse a flow-past area (2a) on one aircraft's supporting wing (2). Third laser sources (7c) intersperse a flow-past area on the other supporting wing (2). Fourth laser sources (7d) intersperse a flow-past area (3a) on the aircraft's tail plane (3).